SW model of the control system of L-159 and L-39NG aircraft including the control laws

other

This work describes a method of designing five control modes of the L159 aircraft. The design of control regulators is created for linearized and separated longitudinal and lateral dynamics. These are supplemented by models of servomechanisms for individual control surfaces. Robust control design is made for a wide range of modes selected from the flight envelope.

31.12.2020

Praha, VZLU